专利名称：Gas turbine combustor, particularly for an
aircraft engine
发明人：Daniele Coutandin申请号：US10118327申请日：20020409公开号：US06810672B2公开日：20041102
专利附图：
摘要：A gas turbine combustor, in particular for an aircraft engine, has at least onechamber, through which combustion gas flows in use, and which is defined by a lateralwall with channeling for feeding cooling air into the chamber and cooling the lateral wall;
part of the channeling is defined by at least one double wall for guiding a relative streamof cooling air into the chamber in a tangential direction with respect to the lateral wall.
申请人：FIATAVIO S.P.A.
代理机构：Shlesinger, Arkwright & Garvey LLP
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